| 00-16-51 |
PZL |
Repetitively replace front tailplane to fuselage joint connector and bushing as specified | PZL-104 |
| 00-16-5 |
Schweizer |
Supersedes 99-17-10 | Identify tail rotor shaft, replace as specified | 330;300C;269,300;269,200 |
| 00-16-4 |
Bell |
Supersedes 97-15-16 | Inspect main rotor adapter assemblies for flapping contact with upper stop plug. Replace as specified | Modify airspeed indicator and RFM as specified | Remove and replace fluidlastic damper blade set as directed | 430 |
| 00-15-9 |
Honeywell Engine |
Remove and inspect applicable HPC impeller as specified | Various models |
| 00-15-52 |
Bell |
Supersedes 00-8-52 | Replace as specified main rotor mast assembly & trunnion | Create component history card as directed | 205, 204B |
| 00-15-51 |
Cessna |
Inspect aileron fairlead tube for protrusion beyond clamp for damage, failure or iregularity | Modify aileron fairlead tubes as specified | 560 XL |
| 00-15-20 |
Agusta |
Perform radiographic inspection of upper and lower surfaces of each main rotor blade for internal corrosion on spar; identify and replace as specified | A109A, II |
| 00-15-19 |
Eurocopter |
Repetitively inspect left and right hand sand filter ejection nozzle for a crack | SA 365N, N1,N2,N3 |
| 00-14-8 |
Piper |
Revise Limitations Section of AFM as specified for activation of ice protection section | Cheyenne 400LS, Cheyenne III |
| 00-14-51 |
Air Tractor |
Superseded by 01-10-4 |
| 00-14-16 |
Bell |
Supersedes 99-6-15 | Install stop on left pedal & placard; adjust specified rigging; install redline VNE of 100 KIAS on all airspeed indicators; report uncommanded right yaw | Replace tail rotor; modify vertical fin & horizontal stabilizer | 407 |
| 00-13-8 |
Eurocopter |
Supersedes 98-15-25 | Conduct tail rotor drive shaft vibration survey and install specified shaft retrofit kit | Install double bearing supports for tail rotor driveshaft and tail boom struts | EC 135 |
| 00-13-1 |
Allison Engine |
Remove and replace stage 1 and stage 2 turbine wheels as specified | Citation X |
| 00-12-9 |
Sikorsky |
Inspect air conditioning soft start assembly | Install retrofit kit as specified | S-76 |
| 00-12-15 |
Dassault |
Superseded by: 04-4-14 |
| 00-11-52 |
Sikorsky |
Inspect rotor blades for span-wise crack | S-76 |
| 00-11-51 |
Tele-Cont |
Superseded by 02-13-4 |
| 00-11-5 |
Air Tractor |
Recurringly inspect fin front spar attachment fittings for fatigue cracks | AT-301,401,501 |
| 00-11-4 |
Commander |
Replace Aeroquip V-band exhaust clamp | 114TC |
| 00-11-3 |
Dassault |
Revise AFM as specified on speed limitations associated with failure of indications of pitch feel system | 2000,900 |
